French passenger jet gone missing from radar screens........
Discussion
Eric Mc said:
julian64 said:
I'll guess lightning strike and the new composite nature of the plane.
Give me an old fashioned aluminium aircraft anyday.
The A330 is mostly an "old fashioned aluminium aircraft". It only uses composites in some components such as the tailfin.Give me an old fashioned aluminium aircraft anyday.
Lighning strikes do not tend to bring airliners down.
I think there is now no doubt that the aircraft broke up at altitude and fell in pieces into the ocean. What caused the breakup will be the central part of the investigation.
Edited by fido on Wednesday 3rd June 09:51
fido said:
Eric Mc said:
julian64 said:
I'll guess lightning strike and the new composite nature of the plane.
Give me an old fashioned aluminium aircraft anyday.
The A330 is mostly an "old fashioned aluminium aircraft". It only uses composites in some components such as the tailfin.Give me an old fashioned aluminium aircraft anyday.
Lighning strikes do not tend to bring airliners down.
I think there is now no doubt that the aircraft broke up at altitude and fell in pieces into the ocean. What caused the breakup will be the central part of the investigation.
Edited by fido on Wednesday 3rd June 09:51
fido said:
Eric Mc said:
julian64 said:
I'll guess lightning strike and the new composite nature of the plane.
Give me an old fashioned aluminium aircraft anyday.
The A330 is mostly an "old fashioned aluminium aircraft". It only uses composites in some components such as the tailfin.Give me an old fashioned aluminium aircraft anyday.
Lighning strikes do not tend to bring airliners down.
I think there is now no doubt that the aircraft broke up at altitude and fell in pieces into the ocean. What caused the breakup will be the central part of the investigation.
Edited by fido on Wednesday 3rd June 09:51
No aircraft is immune from structural failure. However, the designers' task is to ensure that structural limits are not reached in normal day to day operations and over the normal expected working life of the airframe - which could be up to 30 years of service. I cannot think of any airliner designed since around 1960 that has suffered unexpected catastrophic structural failure caused by a design oversight.
The most infanous example is that of the De Havilland Comet 1 airliner which was designed in the mid 1940s. It had inherent flaws in its design which made it vulnerable to fatigue failure of the fuselage skin. These failures caused two separate explosive decopmpressions in airline service which eventually resulted in the Comet 1 being permananetly withdrawn from airline service.
The other example I can think of is that of the Lockheed Electra turboprop. A number of these aircraft experienced main wing spar failure (and total loss of aircraft) when an unexpected resonance between the engines and the metal in the spar developed at certain power settings causing the wings to fail and fall off.
The problem was solved and the Electras were modified and returned to service. Indeed, the military version of the Electra, the Lockheed Orion, continues in service to this day.
However, ANY aircraft can experience catastrophic structural failure if it experiences extreme turbulence or enters a situation where control is lost to such an extent that limiting speeds and G loadings are exceeded.
The most infanous example is that of the De Havilland Comet 1 airliner which was designed in the mid 1940s. It had inherent flaws in its design which made it vulnerable to fatigue failure of the fuselage skin. These failures caused two separate explosive decopmpressions in airline service which eventually resulted in the Comet 1 being permananetly withdrawn from airline service.
The other example I can think of is that of the Lockheed Electra turboprop. A number of these aircraft experienced main wing spar failure (and total loss of aircraft) when an unexpected resonance between the engines and the metal in the spar developed at certain power settings causing the wings to fail and fall off.
The problem was solved and the Electras were modified and returned to service. Indeed, the military version of the Electra, the Lockheed Orion, continues in service to this day.
However, ANY aircraft can experience catastrophic structural failure if it experiences extreme turbulence or enters a situation where control is lost to such an extent that limiting speeds and G loadings are exceeded.
Legend83 said:
mattdaniels said:
Quite a few examples since the Comet. Google for Aloha airlines flight 243 if you want an example.
That is unbelievable! Can't believe they managed to fly all the way back to the airport with loads of passengers exposed.It was caused by the fact that, in terms of pressurisation cycles, that particular aircraft was the "oldest" operating 737 at that time AND it had performed all its work in a damp, salt water environment (i.e. island hopping in Hawaii).
This accelerated the corrosion process beyond the norm.
Eric Mc said:
The other example I can think of is that of the Lockheed Electra turboprop. A number of these aircraft experienced main wing spar failure (and total loss of aircraft) when an unexpected resonance between the engines and the metal in the spar developed at certain power settings causing the wings to fail and fall off.
The problem was solved and the Electras were modified and returned to service. Indeed, the military version of the Electra, the Lockheed Orion, continues in service to this day.
Aside from the obvious tragic circumstances, the worst part of this disaster is that it may be impossible to fully conclude on what the cause was and therefore make any constructive improvements to avoid the 'cause' in the future.
Unless they can trace the majority of bits from the aircraft it is pot luck if they find the key areas.
Unless they can trace the majority of bits from the aircraft it is pot luck if they find the key areas.
Eric Mc said:
Legend83 said:
mattdaniels said:
Quite a few examples since the Comet. Google for Aloha airlines flight 243 if you want an example.
That is unbelievable! Can't believe they managed to fly all the way back to the airport with loads of passengers exposed.It was caused by the fact that, in terms of pressurisation cycles, that particular aircraft was the "oldest" operating 737 at that time AND it had performed all its work in a damp, salt water environment (i.e. island hopping in Hawaii).
This accelerated the corrosion process beyond the norm.
Rach* said:
Legend83 said:
mattdaniels said:
Quite a few examples since the Comet. Google for Aloha airlines flight 243 if you want an example.
That is unbelievable! Can't believe they managed to fly all the way back to the airport with loads of passengers exposed.What a view those passengers must have had from the air!
Traveller said:
Eric Mc said:
The other example I can think of is that of the Lockheed Electra turboprop. A number of these aircraft experienced main wing spar failure (and total loss of aircraft) when an unexpected resonance between the engines and the metal in the spar developed at certain power settings causing the wings to fail and fall off.
The problem was solved and the Electras were modified and returned to service. Indeed, the military version of the Electra, the Lockheed Orion, continues in service to this day.
If anything, metal aircraft of the 1930s were definitely over enginered - mainly because metal, stressed skin construction was brand new at the time and they erred on the side of caution.
Rob P said:
A few websites say the black box "might" float.
Surely it should be designed to float as a major design requirement?! Where is it usually located? I guess the risk is that it goes down with the aircraft and sinks.
Erm, I thought it was made of reinforced material and ridiculously heavy to protect it on impact? Not sure it would float.Surely it should be designed to float as a major design requirement?! Where is it usually located? I guess the risk is that it goes down with the aircraft and sinks.
Legend83 said:
Rob P said:
A few websites say the black box "might" float.
Surely it should be designed to float as a major design requirement?! Where is it usually located? I guess the risk is that it goes down with the aircraft and sinks.
Erm, I thought it was made of reinforced material and ridiculously heavy to protect it on impact? Not sure it would float.Surely it should be designed to float as a major design requirement?! Where is it usually located? I guess the risk is that it goes down with the aircraft and sinks.
There is also a similar device containing the cockpit voice recorder.
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